DocumentCode
1657210
Title
The Stability Analysis of a Controlled Spacecraft with a Retractable Flexible Appendage
Author
Shaoping, Shen ; Hongxin, Wu ; Zhibin, Li
Author_Institution
Beijing Inst. of Control Eng., Beijing
fYear
2007
Firstpage
93
Lastpage
97
Abstract
The controlled spacecraft with a retractable flexible appendage may be unstable during retraction of appendage because of the improper rate of retraction designed. In this paper, according to the Lyapunov second method, the sufficient conditions which guarantee the stability of the system controlled by the PD law in retracting phase are deduced. These conditions are instructive for designing the proper rate of retraction and control law to satisfy the stabilization requirement of this system.
Keywords
Lyapunov methods; PD control; aerospace control; space vehicles; stability; Lyapunov second method; PD law; controlled spacecraft; retractable flexible appendage; retraction; stability; Aerospace engineering; Control systems; Design engineering; PD control; Space vehicles; Stability analysis; Sufficient conditions; Lyapunov second method; Retractable flexible; Spacecraft; appendage;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference, 2007. CCC 2007. Chinese
Conference_Location
Hunan
Print_ISBN
978-7-81124-055-9
Electronic_ISBN
978-7-900719-22-5
Type
conf
DOI
10.1109/CHICC.2006.4347588
Filename
4347588
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